Robust autopilot design with maximum stability radius
This paper presents the robust control design for aircraft autopilot. The controller provides a maximum stability radius to the closed-loop system. The technique uses the notion of complex stability radius and the Linear Matrix Inequalities (LMI) to obtain the feedback controller gain. The technique...
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2007
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my.iium.irep.52932012-05-23T01:22:06Z http://irep.iium.edu.my/5293/ Robust autopilot design with maximum stability radius Akmeliawati, Rini Kuang, Ye Chow TJ212 Control engineering TK Electrical engineering. Electronics Nuclear engineering This paper presents the robust control design for aircraft autopilot. The controller provides a maximum stability radius to the closed-loop system. The technique uses the notion of complex stability radius and the Linear Matrix Inequalities (LMI) to obtain the feedback controller gain. The technique is illustrated on a feedback controller of an autopilot system of a twin engine civil aircraft. The results is compared to those that are obtained using a linear quadratic regulator (LQR) technique. 2007 Conference or Workshop Item REM application/pdf en http://irep.iium.edu.my/5293/1/icit2006.pdf Akmeliawati, Rini and Kuang, Ye Chow (2007) Robust autopilot design with maximum stability radius. In: IEEE International Conference on Industrial Technology, 2006. ICIT 2006., 15-17 Dec, 2006, Mumbai. http://dx.doi.org/10.1109/ICIT.2006.372330 doi:10.1109/ICIT.2006.372330 |
| institution |
Universiti Islam Antarabangsa Malaysia |
| building |
IIUM Library |
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Institutional Repository |
| continent |
Asia |
| country |
Malaysia |
| content_provider |
International Islamic University Malaysia |
| content_source |
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http://irep.iium.edu.my/ |
| language |
English |
| topic |
TJ212 Control engineering TK Electrical engineering. Electronics Nuclear engineering |
| spellingShingle |
TJ212 Control engineering TK Electrical engineering. Electronics Nuclear engineering Akmeliawati, Rini Kuang, Ye Chow Robust autopilot design with maximum stability radius |
| description |
This paper presents the robust control design for aircraft autopilot. The controller provides a maximum stability radius to the closed-loop system. The technique uses the notion of complex stability radius and the Linear Matrix Inequalities (LMI) to obtain the feedback controller gain. The technique is illustrated on a feedback controller of an autopilot system of a twin engine civil aircraft. The results is compared to those that are obtained using a linear quadratic regulator (LQR) technique. |
| format |
Conference or Workshop Item |
| author |
Akmeliawati, Rini Kuang, Ye Chow |
| author_facet |
Akmeliawati, Rini Kuang, Ye Chow |
| author_sort |
Akmeliawati, Rini |
| title |
Robust autopilot design with maximum stability radius |
| title_short |
Robust autopilot design with maximum stability radius |
| title_full |
Robust autopilot design with maximum stability radius |
| title_fullStr |
Robust autopilot design with maximum stability radius |
| title_full_unstemmed |
Robust autopilot design with maximum stability radius |
| title_sort |
robust autopilot design with maximum stability radius |
| publishDate |
2007 |
| url |
http://irep.iium.edu.my/5293/1/icit2006.pdf http://irep.iium.edu.my/5293/ http://dx.doi.org/10.1109/ICIT.2006.372330 |
| _version_ |
1643605509490606080 |
| score |
13.251813 |